CZ-4B R/B

Satellite information

Favourite Embed

Satellite Type and Status

ROCKET BODYIN ORBIT

Key statistics

Satellite CZ-4B R/B at a glance.

Uptime

7931

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.7

Latest

Satellite identification and parameters

Extended collection of information and parameters for CZ-4B R/B.

Object identification

Identified? True

Debris? False

Object name: CZ-4B R/B

International designator: 2003-049C

Object number (NORAD): 28059

Object ID (CCSDS): 28059

Country: PEOPLES REPUBLIC OF CHINA (PRC)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 98.989 minutes

Inclination: 98.6601 deg

SMA: 7088.468 km

Apoapsis: 743.818 km

Periapsis: 676.849 km

RAAN: 169.6386 deg

Eccentricy: 0.0047238

Argument of periapsis: 258.6094 deg

Mean anomaly: 100.9793 deg

Mean motion: 14.54702372 rev/day

Mean motion (dot): 0.00000223 rev/day2

B* drag term: 0.0000634 1/REarth

Two-line elements (TLE)

Creation date: July 8, 2025, 2:27 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 7, 2025, 9:16 p.m. UTC

TLE line 0: 0 CZ-4B R/B

TLE line 1: 1 28059U 03049C 25188.88658112 .00000223 00000-0 63400-4 0 9997

TLE line 2: 2 28059 98.6601 169.6386 0047238 258.6094 100.9793 14.54702372151004

Live tracking on map

Real-time ground track for satellite CZ-4B R/B.

In-orbit conjunctions

A list of the most updated potential collisions computed for object CZ-4B R/B.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-06-15 03:15:42 0.0001527408 425.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-12-13 21:49:29 0.0004283221 346.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-09 04:43:45 0.0001446308 475.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-07-22 20:46:19 0.0001486641 287.0 (m) DEBRIS

Associated space launch

The satellite is China's first operational civilian remote-sensing satellite, specifically designed for the Chinese Ministry of Land and Resources (MLR).

CZ-4B R/B was lifted into orbit during the mission ‘Long March 4B | Zi Yuan 1-2’, on board a Long March 4B space rocket.

The launch took place on Oct. 21, 2003, 3:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 4B | Zi Yuan 1-2
Long March 4B | Zi Yuan 1-2

Agency: N/A

Status: Launch Successful

Launch date: Oct. 21, 2003, 3:16 a.m. UTC

Rocket: Long March 4B

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.